CN116806013A - Message transmission method and corresponding terminal - Google Patents

Message transmission method and corresponding terminal Download PDF

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Publication number
CN116806013A
CN116806013A CN202210270407.0A CN202210270407A CN116806013A CN 116806013 A CN116806013 A CN 116806013A CN 202210270407 A CN202210270407 A CN 202210270407A CN 116806013 A CN116806013 A CN 116806013A
Authority
CN
China
Prior art keywords
satellite
terminal
message
interface
identifier
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202210270407.0A
Other languages
Chinese (zh)
Inventor
林子杰
张若兰
钱锋
周道洋
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Huawei Technologies Co Ltd
Original Assignee
Huawei Technologies Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Huawei Technologies Co Ltd filed Critical Huawei Technologies Co Ltd
Priority to CN202210270407.0A priority Critical patent/CN116806013A/en
Priority to EP23736591.1A priority patent/EP4274270A1/en
Priority to US18/552,285 priority patent/US20240048651A1/en
Priority to PCT/CN2023/080660 priority patent/WO2023174161A1/en
Publication of CN116806013A publication Critical patent/CN116806013A/en
Pending legal-status Critical Current

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Classifications

    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/1851—Systems using a satellite or space-based relay
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04B—TRANSMISSION
    • H04B7/00—Radio transmission systems, i.e. using radiation field
    • H04B7/14—Relay systems
    • H04B7/15—Active relay systems
    • H04B7/185—Space-based or airborne stations; Stations for satellite systems
    • H04B7/1853—Satellite systems for providing telephony service to a mobile station, i.e. mobile satellite service
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/72—Mobile telephones; Cordless telephones, i.e. devices for establishing wireless links to base stations without route selection
    • H04M1/724—User interfaces specially adapted for cordless or mobile telephones
    • H04M1/72403—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality
    • H04M1/7243—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality with interactive means for internal management of messages
    • H04M1/72436—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality with interactive means for internal management of messages for text messaging, e.g. SMS or e-mail
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W4/00—Services specially adapted for wireless communication networks; Facilities therefor
    • H04W4/12—Messaging; Mailboxes; Announcements
    • H04W4/14—Short messaging services, e.g. short message services [SMS] or unstructured supplementary service data [USSD]
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W64/00—Locating users or terminals or network equipment for network management purposes, e.g. mobility management
    • H04W64/003—Locating users or terminals or network equipment for network management purposes, e.g. mobility management locating network equipment
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/72—Mobile telephones; Cordless telephones, i.e. devices for establishing wireless links to base stations without route selection
    • H04M1/724—User interfaces specially adapted for cordless or mobile telephones
    • H04M1/72448—User interfaces specially adapted for cordless or mobile telephones with means for adapting the functionality of the device according to specific conditions
    • H04M1/72457—User interfaces specially adapted for cordless or mobile telephones with means for adapting the functionality of the device according to specific conditions according to geographic location
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04W—WIRELESS COMMUNICATION NETWORKS
    • H04W84/00—Network topologies
    • H04W84/02—Hierarchically pre-organised networks, e.g. paging networks, cellular networks, WLAN [Wireless Local Area Network] or WLL [Wireless Local Loop]
    • H04W84/04—Large scale networks; Deep hierarchical networks
    • H04W84/06—Airborne or Satellite Networks

Abstract

The application discloses a message transmission method which is applied to a terminal. The method comprises the following steps: the terminal can display a satellite finding guiding interface, the satellite finding guiding interface comprises a satellite identifier, the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relation between the terminal and a target satellite, the terminal can respond to the mobile operation of a user on the terminal, the display position of the satellite identifier is updated, and if the position relation between the terminal after the mobile operation and the target satellite meets the message transmission condition, the terminal sends satellite information to the target satellite or receives satellite information from the target satellite. The scheme provided by the application can guide the user to adjust the position between the terminal and the target satellite through the satellite finding guiding interface, so that the terminal can quickly send or receive satellite information.

Description

Message transmission method and corresponding terminal
Technical Field
The application relates to the technical field of communication, in particular to a message transmission method and a corresponding terminal.
Background
Short message (short message) is a basic service for communication between terminals (e.g. mobile phones), and typically a transmitting terminal may send a short message through an access network device (e.g. a first base station), where the short message is forwarded to the access network device (e.g. a second base station) to which the receiving terminal is connected via a network, and then send the short message to the receiving terminal through the second base station.
Disclosure of Invention
The application provides a message transmission method, which is used for guiding a user to adjust the position relation between a terminal and a target satellite through a satellite finding guiding interface, so that the terminal can quickly send or receive satellite messages. The application also provides a corresponding terminal, a computer readable storage medium, a computer program product and the like.
The first aspect of the present application provides a method for transmitting a message, which is applied to a terminal, and includes: displaying a satellite finding guiding interface, wherein the satellite finding guiding interface comprises a satellite identifier, and the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relationship between the terminal and a target satellite; responding to the mobile operation of the user to the terminal, and updating the display position of the satellite identifier; and if the position relation between the mobile terminal and the target satellite meets the message transmission condition, sending the first satellite message to the target satellite or receiving the first satellite message from the target satellite.
In the application, the star finding guiding interface is used for guiding the user to adjust the position of the terminal. The user can determine the position relationship between the terminal and the target satellite through the display position of the satellite identifier in the satellite searching guide interface, and then the mobile terminal (such as a leftward or rightward mobile terminal and an upward or downward mobile terminal) responds to the movement to adjust the display position of the satellite identifier on the satellite searching guide interface.
In the application, the condition that the position relation between the mobile terminal and the target satellite meets the message transmission condition can be that the position relation between the mobile terminal and the target satellite can enable the terminal to establish communication connection with the target satellite.
In the application, satellite message refers to a message which is directly sent to a satellite by a terminal or a message which is directly sent to the terminal by the satellite, and the message does not need to be forwarded by a base station.
In the first aspect, the terminal may guide the user to adjust the position relationship between the terminal and the target satellite through the satellite finding guiding interface, so that the terminal may quickly establish communication connection with the satellite, and thus the terminal may quickly send or receive satellite messages.
In a possible implementation manner of the first aspect, the star finding guiding interface further includes a star finding prompt message, where the star finding prompt message is used to prompt a direction of the mobile terminal of the user.
In this possible implementation manner, the star finding prompt information is used for prompting the direction of the mobile terminal of the user. If the satellite finding prompt information is a leftward mobile terminal, a rightward mobile terminal, an upward mobile terminal or a downward mobile terminal. The satellite finding prompt information is usually a prompt given by the terminal according to the shortest moving path, so that a user can quickly move the terminal to a position suitable for establishing communication connection with a target satellite according to the satellite finding prompt information, and the speed of sending satellite information to the target satellite or receiving satellite information by the terminal is further increased.
In a possible implementation manner of the first aspect, the star finding guide interface includes a first star finding guide interface and a second star finding guide interface. The first satellite searching guide interface comprises a first satellite identifier and a first alignment area, wherein the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in azimuth, and when the position relation between the terminal and the target satellite in azimuth meets the message transmission condition, the first satellite identifier is located in the first alignment area. The second satellite searching guide interface comprises a second satellite identifier and a second alignment area, wherein the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is positioned in the second alignment area.
In the possible implementation manner, satellite identification and alignment areas are set from two dimensions of azimuth angle and pitch angle of the terminal and the target satellite, so that when the position of the terminal is adjusted, the position relationship between the terminal and the target satellite on the azimuth angle and the pitch angle can be adjusted according to the satellite identification and alignment areas on the first satellite finding guiding interface and the second satellite finding guiding interface respectively, and the speed of establishing communication connection between the terminal and the target satellite can be increased.
In a possible implementation manner of the first aspect, the steps are as follows: displaying a star finding guiding interface; and updating the display position of the satellite identifier in response to the mobile operation of the user on the terminal, specifically comprising: displaying a first satellite finding guiding interface, and updating the display position of a first satellite identifier in response to the leftward movement operation or the rightward movement operation of a user on the terminal; displaying a second satellite finding guiding interface when the first satellite identifier is positioned in the first alignment area; and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
In this possible implementation manner, according to the display sequence of the terminal, the first satellite searching guiding interface is displayed first, and when the first satellite identifier is located in the first alignment area, that is, after the terminal is aligned with the target satellite in azimuth, the second satellite searching guiding interface is displayed, where the second satellite searching guiding interface may not include the first satellite identifier and the first alignment area, or may include the first satellite identifier and the first alignment area. According to the implementation mode, aiming at the star finding guiding interface, the application provides various presentation modes.
In a possible implementation manner of the first aspect, the steps are as follows: displaying a star finding guiding interface; and updating the display position of the satellite identifier in response to the mobile operation of the user on the terminal, specifically comprising: displaying a second satellite finding guiding interface, and updating the display position of a second satellite identifier in response to the upward movement operation or the downward movement operation of a user on the terminal; displaying a first satellite finding guiding interface when the second satellite identifier is positioned in the second alignment area; and updating the display position of the first satellite identifier in response to the leftward or rightward movement operation of the terminal by the user.
In this possible implementation manner, the second satellite finding guiding interface is displayed first according to the display sequence of the terminal, and when the second satellite identifier is located in the second alignment area, that is, after the terminal aligns with the target satellite on the pitch angle, the first satellite finding guiding interface is displayed, where the first satellite finding guiding interface may not include the second satellite identifier and the second alignment area, or may include the second satellite identifier and the second alignment area. According to the implementation mode, aiming at the star finding guiding interface, the application provides various presentation modes.
In a possible implementation manner of the first aspect, the satellite finding guiding interface includes a first satellite identification and a first alignment area, and a second satellite identification and a second alignment area; the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and is positioned in the first alignment area when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition; the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is located in the second alignment area.
In the possible implementation manner, the satellite identification and the alignment area are set from two dimensions of the azimuth angle and the pitch angle of the terminal and the target satellite, so that when the position of the terminal is adjusted, the position relationship between the terminal and the target satellite on the azimuth angle and the pitch angle can be adjusted according to the satellite identification and the alignment area on the satellite finding guiding interface, and the speed of establishing communication connection between the terminal and the target satellite can be increased.
In a possible implementation manner of the first aspect, the steps are as follows: the method for updating the display position of the satellite identifier in response to the mobile operation of the user on the terminal specifically comprises the following steps: responding to the leftward movement operation or rightward movement operation of the user on the terminal, and updating the display position of the first satellite identifier; and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
In this possible implementation manner, the satellite searching guiding interface includes a first satellite identifier and a first alignment area, and when the second satellite identifier and the second alignment area are used, the user can firstly move the terminal leftwards or rightwards, firstly adjust the position relationship between the terminal and the target satellite in the direction angle, then firstly move the terminal upwards or downwards, and adjust the position relationship between the terminal and the target satellite in the pitch angle. Or the terminal is moved upwards or downwards firstly, the position relation between the terminal and the target satellite in the pitch angle is adjusted firstly, and then the terminal is moved leftwards or rightwards firstly, and the position relation between the terminal and the target satellite in the azimuth angle is adjusted. The user can also adjust the position relationship between the azimuth angle and the pitch angle at the same time, for example: an upper left mobile terminal or a lower left mobile terminal, or an upper right mobile terminal or a lower right mobile terminal. The user can guide the mobile terminal according to the star finding prompt information displayed on the terminal. According to the implementation mode, aiming at the star finding guiding interface, the application provides various presentation modes.
In a possible implementation manner of the first aspect, when the display position of the first satellite identifier is located outside the first alignment area, the first alignment area is displayed in a first color; when the display position of the first satellite mark is positioned in the first alignment area, the first alignment area is displayed in a second color, and the first color is different from the second color.
In this possible implementation manner, the position of the terminal and the target satellite in the azimuth angle can be adjusted through color change, so that the user can be better prompted that the terminal has moved to a proper position in the left or right direction.
In a possible implementation manner of the first aspect, when the display position of the second satellite identifier is located outside the second alignment area, the second alignment area is displayed in a third color; when the display position of the second satellite mark is positioned in the second alignment area, the second alignment area is displayed in a fourth color, and the third color is different from the fourth color.
In this possible implementation manner, the position of the terminal on the pitch angle and the target satellite can be adjusted through color change, so that the user can be better prompted that the terminal has moved to a proper position in an upward or downward direction.
In a possible implementation manner of the first aspect, when the terminal is configured to send the first satellite message, before displaying the satellite finding guidance interface, the method further includes: and responding to the operation of newly building the satellite message or replying to the satellite message by the user, displaying a satellite message editing interface, wherein the satellite message editing interface is used for inputting the content of the first satellite message by the user.
In this possible implementation manner, the terminal may configure the satellite message function on the short message application or other communication applications, so as to send the satellite message.
In a possible implementation manner of the first aspect, the steps are as follows: the display of the star finding guiding interface specifically comprises the following steps: and responding to the sending operation of the user on the first satellite message, and displaying a star finding guiding interface.
In this possible implementation manner, the terminal responds to the sending operation of the user to the first satellite message, and displays a satellite finding guiding interface for the user to perform the satellite finding guiding process in the various implementation manners described above.
In a possible implementation manner of the first aspect, when the terminal is configured to receive the first satellite message, the steps are as follows: the display of the star finding guiding interface specifically comprises the following steps: and responding to the operation of receiving the satellite message by the user, and displaying a star finding guiding interface.
In this possible implementation manner, when receiving the satellite message, the terminal responds to the operation of the user to receive the satellite message, and displays a satellite finding guiding interface for the user to perform the satellite finding guiding process in the various implementation manners described above.
In a possible implementation manner of the first aspect, when the terminal is configured to send the first satellite message, before displaying the satellite finding guidance interface, the method further includes: sending a common message to a base station; receiving a response message of failure of sending the common message; the steps are as follows: the display of the star finding guiding interface specifically comprises the following steps: and responding to the response message of failure of sending the common message, and displaying a star finding guiding interface.
In this possible implementation, the common message refers to a message sent through the base station. After the common message is sent failure, the content of the common message can be transferred to a satellite message editing interface, and the content of the common message is sent through the satellite message. In this way, the success rate of message transmission can be improved.
In a possible implementation manner of the first aspect, after sending the first satellite message, the method further includes: determining a position change after the terminal transmits the first satellite message in response to a user transmitting operation of the second satellite message; if the position change after the terminal sends the first satellite message is smaller than the first threshold value, the terminal sends the second satellite message to the target satellite, and the satellite finding guiding interface is not displayed.
In this possible implementation manner, the first threshold may be preconfigured, and when the first satellite message is sent, the user adjusts the position relationship between the terminal and the target satellite, and establishes the communication connection between the terminal and the target satellite, so that the user can keep the position, send the second satellite message to the same recipient or different recipients, and does not need to display the satellite finding guiding interface any more, thereby improving the speed of sending the satellite message.
In addition, as a possible implementation manner, after the first satellite message is sent, the method further includes: determining a time when the terminal transmits the first satellite message in response to a transmission operation of the user on the second satellite message; if the time difference between the time distance when the terminal sends the first satellite message and the time distance when the user triggers the sending operation of the second satellite message is smaller than a second threshold value, the second satellite message is sent to the target satellite, and the satellite finding guiding interface is not displayed.
In a possible implementation manner of the first aspect, after the sending of the first satellite message to the target satellite, the method further includes: receiving a response message of failure of the first satellite message transmission; and displaying the star finding guiding interface according to the response message of the failure of the first satellite message transmission.
In this possible implementation, if the first satellite message fails to be sent, it indicates that the communication connection between the terminal and the target satellite is disconnected or the signal is poor, and the positional relationship between the terminal and the target satellite needs to be adjusted again.
A second aspect of the present application provides a terminal, comprising:
the display unit is used for displaying a satellite finding guiding interface, the satellite finding guiding interface comprises a satellite identifier, and the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relation between the terminal and the target satellite.
And the processing unit is used for responding to the mobile operation of the user on the terminal and updating the display position of the satellite identifier displayed by the display unit.
And the receiving and transmitting unit is used for transmitting the first satellite message to the target satellite or receiving the first satellite message from the target satellite if the position relation between the mobile terminal and the target satellite meets the message transmission condition.
In a possible implementation manner of the second aspect, the star finding guiding interface further includes a star finding prompt information, where the star finding prompt information is used to prompt a direction of the mobile terminal of the user.
In a possible implementation manner of the second aspect, the star finding guide interface includes a first star finding guide interface and a second star finding guide interface; the first satellite searching guide interface comprises a first satellite identifier and a first alignment area, wherein the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition, the first satellite identifier is positioned in the first alignment area; the second satellite searching guide interface comprises a second satellite identifier and a second alignment area, wherein the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is positioned in the second alignment area.
In a possible implementation manner of the second aspect, the display unit is specifically configured to display the first star finding guidance interface.
The processing unit is specifically configured to update the display position of the first satellite identifier in response to a leftward movement operation or a rightward movement operation of the terminal by the user.
The display unit is specifically configured to display the second satellite finding guiding interface when the first satellite identifier is located in the first alignment area.
And the processing unit is specifically used for updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
In a possible implementation manner of the second aspect, the display unit is specifically configured to display the second star finding guidance interface.
And the processing unit is specifically used for updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
The display unit is specifically configured to display the first satellite finding guiding interface when the second satellite identifier is located in the second alignment area.
The processing unit is specifically configured to update the display position of the first satellite identifier in response to a leftward movement or rightward movement operation of the terminal by the user.
In a possible implementation manner of the second aspect, the satellite finding guiding interface includes a first satellite identification and a first alignment area, and a second satellite identification and a second alignment area; the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and is positioned in the first alignment area when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition; the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is located in the second alignment area.
In a possible implementation manner of the second aspect, the processing unit is specifically configured to update the display position of the first satellite identifier in response to a leftward movement operation or a rightward movement operation of the terminal by the user; and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
In a possible implementation manner of the second aspect, when the display position of the first satellite identifier is located outside the first alignment area, the first alignment area is displayed in a first color; when the display position of the first satellite mark is positioned in the first alignment area, the first alignment area is displayed in a second color, and the first color is different from the second color.
In a possible implementation manner of the second aspect, when the display position of the second satellite identifier is located outside the second alignment area, the second alignment area is displayed in a third color; when the display position of the second satellite mark is positioned in the second alignment area, the second alignment area is displayed in a fourth color, and the third color is different from the fourth color.
In a possible implementation manner of the second aspect, the display unit is further configured to, when the terminal is configured to send the first satellite message, display a satellite message editing interface, before displaying the satellite-finding guiding interface, in response to an operation of creating the satellite message by the user or an operation of replying to the satellite message, where the satellite message editing interface is configured to be used by the user to input the content of the first satellite message.
In a possible implementation manner of the second aspect, the display unit is specifically configured to display the satellite finding guidance interface in response to a sending operation of the first satellite message by the user.
In a possible implementation manner of the second aspect, the display unit is specifically configured to display the star finding guidance interface in response to an operation of receiving the satellite message by the user.
In a possible implementation manner of the second aspect, the transceiver unit is further configured to send a common message to the base station; and receiving a response message of failure of sending the common message.
The display unit is specifically used for responding to the response message of the failure of the common message transmission and displaying the star finding guiding interface.
In a possible implementation manner of the second aspect, the processing unit is further configured to determine a change in position after the terminal transmits the first satellite message in response to a transmission operation of the second satellite message by the user.
And the receiving and transmitting unit is also used for transmitting a second satellite message to the target satellite if the position change after the terminal transmits the first satellite message is smaller than the first threshold value, and the satellite finding guiding interface is not displayed.
In a possible implementation manner of the second aspect, the transceiver unit is further configured to receive a response message that the first satellite message fails to be sent.
And the display unit is also used for displaying the star finding guiding interface according to the response message of the failure of the first satellite message transmission.
A third aspect of the present application provides a terminal for performing the method of the first aspect or any possible implementation of the first aspect.
A fourth aspect of the application provides a chip system comprising one or more interface circuits and one or more processors; the interface circuit and the processor are interconnected through a circuit; the interface circuit is used for receiving signals from the memory of the terminal and sending signals to the processor, and the signals comprise computer instructions stored in the memory; when the processor executes the computer instructions, the terminal performs the method of the first aspect or any possible implementation of the first aspect.
A fifth aspect of the application provides a computer readable storage medium having stored thereon a computer program or instructions which, when run on a computer, cause the computer to perform the method of the first aspect or any possible implementation of the first aspect.
A sixth aspect of the application provides a computer program product comprising computer program code which, when executed on a computer, causes the computer to perform the method of the first aspect or any of the possible implementations of the first aspect.
The technical effects of the second, third, fourth, fifth, and sixth aspects or any one of the possible implementation manners of the second, third, fourth, fifth, and sixth aspects may be referred to the technical effects of the first aspect or the different possible implementation manners of the first aspect, which are not described herein.
Drawings
FIG. 1A is a schematic diagram of an application scenario provided in an embodiment of the present application;
fig. 1B is another schematic diagram of an application scenario provided in an embodiment of the present application;
fig. 1C is another schematic diagram of an application scenario provided in an embodiment of the present application;
fig. 1D is another schematic diagram of an application scenario provided in an embodiment of the present application;
fig. 1E is another schematic diagram of an application scenario provided in an embodiment of the present application;
fig. 2 is a schematic structural diagram of a terminal according to an embodiment of the present application;
FIG. 3 is a schematic diagram of an embodiment of a method for sending a message according to an embodiment of the present application;
FIG. 4A is a schematic diagram of an interface according to an embodiment of the present application;
FIG. 4B is a schematic diagram of an interface for information provided by an embodiment of the present application;
FIG. 4C is a schematic diagram of an interface of a satellite SMS according to an embodiment of the present application;
FIG. 4D is an interface diagram of a newly created satellite message according to an embodiment of the present application;
FIG. 5A is a diagram of a loading interface of a star finder according to the present application;
FIG. 5B is a schematic diagram of a three-dimensional coordinate system provided by an embodiment of the present application;
FIGS. 5C-5F are schematic diagrams illustrating a star-finding guidance interface according to embodiments of the present application;
FIGS. 6A-6D are schematic diagrams of a star-finding guidance interface according to embodiments of the present application;
fig. 7A to fig. 7C are schematic diagrams of a star-finding guidance interface according to an embodiment of the application;
FIGS. 8A-8C are schematic diagrams of a star-finding guidance interface according to embodiments of the present application;
FIG. 9 is another schematic diagram of a star finding guidance interface provided by an embodiment of the present application;
FIGS. 10A-10D are schematic diagrams of a star-finding guidance interface according to embodiments of the present application;
FIG. 11A is a schematic diagram of a satellite message editing interface according to an embodiment of the present application;
FIG. 11B is another schematic diagram of a satellite message editing interface provided by an embodiment of the present application;
FIG. 11C is another schematic diagram of a satellite message editing interface provided by an embodiment of the present application;
FIG. 11D is another schematic diagram of a satellite message editing interface provided by an embodiment of the present application;
FIG. 11E is another schematic diagram of a satellite message editing interface provided by an embodiment of the present application;
FIG. 12 is a diagram of an embodiment of a method for message reception provided by an embodiment of the present application;
Fig. 13A is another interface schematic diagram of a satellite short message according to an embodiment of the present application;
fig. 13B is another interface schematic diagram of a satellite short message according to an embodiment of the present application;
fig. 14 is another schematic structural diagram of a terminal according to an embodiment of the present application.
Detailed Description
Embodiments of the present application will now be described with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the present application. As one of ordinary skill in the art can know, with the development of technology and the appearance of new scenes, the technical scheme provided by the embodiment of the application is also applicable to similar technical problems.
The terms first, second and the like in the description and in the claims and in the above-described figures, are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used may be interchanged where appropriate such that the embodiments described herein may be implemented in other sequences than those illustrated or otherwise described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
The embodiment of the application provides a message transmission method, which is used for guiding a user to adjust the position relation between a terminal and a target satellite through a satellite finding guiding interface, so that the terminal can quickly send or receive satellite messages. The application also provides a corresponding terminal, a computer readable storage medium, a computer program product and the like. The following will describe in detail.
Before describing the method provided by the embodiment of the present application, an application scenario of the method provided by the embodiment of the present application is described. The application scenario of the method provided by the embodiment of the application can be shown in fig. 1A to 1E. Fig. 1A, 1B, and 1C show application scenarios for transmitting satellite messages, and fig. 1C, 1D, and 1E show application scenarios for receiving satellite messages.
In the embodiment of the application, the satellite message refers to a message which is directly sent to the satellite by the terminal or a message which is directly received from the satellite by the terminal. If the message between the terminal and the satellite needs to be transferred through other devices (such as a base station or a cloud network), the message is called a common message.
In the embodiment of the application, the satellite message function item can be configured in the message application or other communication applications of the terminal, and the user can edit the satellite message through the satellite message function item on the terminal and click the sending operation, so that the terminal sends the satellite message to the satellite. Alternatively, the user may click on the receiving operation of the satellite message through the satellite message function item at the terminal, and the terminal receives the satellite message from the satellite.
Note that, the message application refers to an application for sending or receiving a message (SM), and the other communication applications may be instant messaging applications or other applications capable of receiving or sending a message.
An application scenario for transmitting satellite messages as shown in fig. 1A, the application scenario (or architecture) may include: a first terminal, a satellite, a base station, and a second terminal. The first terminal sends satellite information to the satellite, the satellite sends the content of the satellite information to the base station after receiving the satellite information, the base station sends the content of the satellite information to the second terminal, and the second terminal displays the content of the satellite information in a common message after receiving the content of the satellite information.
An application scenario for transmitting satellite messages is illustrated in fig. 1B. The application scenario (or architecture) may include: the system comprises a first terminal, a satellite, a cloud network and a second terminal, wherein the first terminal sends satellite information to the satellite, the satellite sends the content of the satellite information to the cloud network after receiving the satellite information, the cloud network sends the content of the satellite information to the second terminal, the second terminal receives the content of the satellite information through the cloud network, and the content of the satellite information can be displayed in a common message of a corresponding application (App).
An application scenario for transmitting satellite messages and receiving satellite messages as shown in fig. 1C, the application scenario (or architecture) may include: the satellite information receiving device comprises a first terminal, a satellite and a second terminal, wherein the first terminal sends satellite information to the satellite, the satellite sends the satellite information to the second terminal after receiving the satellite information, and the second terminal displays the satellite information after receiving the satellite information from the satellite.
An application scenario for receiving satellite messages as shown in fig. 1D, the application scenario (or architecture) may include: a first terminal, a base station, a satellite, and a second terminal. The method comprises the steps that a first terminal sends a common message to a base station, the base station sends the common message to a satellite, after the satellite receives the common message, the content of the common message is sent to a second terminal, and after the second terminal receives the content of the common message, the content of the common message is displayed in a satellite message function item in a satellite message mode.
Satellite messages are received as shown in fig. 1E. The application scenario (or architecture) may include: the cloud network receives the common message, then sends the common message to the satellite, and after receiving the common message, the satellite sends the content of the common message to the second terminal, and after receiving the content of the common message, the second terminal displays the content of the common message in the satellite message function item in the form of a satellite message.
In the above, only one satellite is illustrated in the scenario shown in fig. 1A to 1E, in fact, the above process may also involve multiple satellites, for example, two satellites, where after one satellite receives a satellite message from a first terminal, the satellite message may be sent to another satellite, and the other satellite sends the satellite message to a second terminal or other devices (such as a base station or a cloud network).
The first terminal and the second terminal described above may be digital display products such as a mobile phone, a tablet computer (pad), a portable game machine, a palm computer (personal digital assistant, PDA), a notebook computer, an ultra mobile personal computer (ultra mobile personal computer, UMPC), a handheld computer, a netbook, a vehicle-mounted media playing device, a wearable electronic device, a Virtual Reality (VR) terminal device, an Augmented Reality (AR) terminal device, and the like. The embodiment of the application is described by taking the example that the first terminal and the second terminal are mobile phones.
Fig. 2 is a schematic structural diagram of a terminal according to an embodiment of the present application. As shown in fig. 2, the terminal may include a processor 210, an external memory interface 220, an internal memory 221, a universal serial bus (universal serial bus, USB) interface 230, a charge management module 240, a power management module 241, a battery 242, an antenna 1, an antenna 2, an antenna 3, a mobile communication module 250, a satellite communication module 251, a wireless communication module 260, an audio module 270, a speaker 270A, a receiver 270B, a microphone 270C, an earphone interface 270D, a sensor module 280, keys 290, a motor 291, an indicator 292, a camera 293, a display 294, a subscriber identity module (subscriber identification module, SIM) card interface 295, and the like. Among other things, the sensor module 280 may include a pressure sensor 280A, a gyroscope sensor 280B, a barometric pressure sensor 280C, a magnetic sensor 280D, an acceleration sensor 280E, a distance sensor 280F, a proximity light sensor 280G, a fingerprint sensor 280H, a temperature sensor 280J, a touch sensor 280K, an ambient light sensor 280L, a bone conduction sensor 280M, a motion sensor 280N, and the like.
It will be appreciated that the structure illustrated in this embodiment does not constitute a specific limitation on the terminal. In other embodiments, the terminal may include more or fewer components than shown, or certain components may be combined, or certain components may be split, or different arrangements of components. The illustrated components may be implemented in hardware, software, or a combination of software and hardware.
Processor 210 may include one or more processing units such as, for example: the processor 210 may include an application processor (application processor, AP), a modem processor, a graphics processor (graphics processing unit, GPU), an image signal processor (image signal processor, ISP), a controller, a memory, a video codec, a digital signal processor (digital signal processor, DSP), a baseband processor, and/or a neural network processor (neural-network processing unit, NPU), etc. Wherein the different processing units may be separate devices or may be integrated in one or more processors.
The controller may be a neural hub and command center of the terminal. The controller can generate operation control signals according to the instruction operation codes and the time sequence signals to finish the control of instruction fetching and instruction execution.
A memory may also be provided in the processor 210 for storing instructions and data. In some embodiments, the memory in the processor 210 is a cache memory. The memory may hold instructions or data that the processor 210 has just used or recycled. If the processor 210 needs to reuse the instruction or data, it may be called directly from the memory. Repeated accesses are avoided and the latency of the processor 210 is reduced, thereby improving the efficiency of the system.
In some embodiments, processor 210 may include one or more interfaces. The interfaces may include an integrated circuit (inter-integrated circuit, I2C) interface, an integrated circuit built-in audio (inter-integrated circuit sound, I2S) interface, a pulse code modulation (pulse code modulation, PCM) interface, a universal asynchronous receiver transmitter (universal asynchronous receiver/transmitter, UART) interface, a mobile industry processor interface (mobile industry processor interface, MIPI), a general-purpose input/output (GPIO) interface, a subscriber identity module (subscriber identity module, SIM) interface, and/or a universal serial bus (universal serial bus, USB) interface, among others.
It should be understood that the connection relationship between the modules illustrated in this embodiment is only illustrative, and does not limit the structure of the terminal. In other embodiments, the terminal may also use different interfacing manners in the foregoing embodiments, or a combination of multiple interfacing manners.
The charge management module 240 is configured to receive a charge input from a charger. The charger can be a wireless charger or a wired charger. In some wired charging embodiments, the charge management module 240 may receive a charging input of a wired charger through the USB interface 230. In some wireless charging embodiments, the charge management module 240 may receive wireless charging input through a wireless charging coil of the terminal. The charging management module 240 may also supply power to the terminal through the power management module 241 while charging the battery 242.
The power management module 241 is used for connecting the battery 242, and the charge management module 240 and the processor 210. The power management module 241 receives input from the battery 242 and/or the charge management module 240 and provides power to the processor 210, the internal memory 221, the external memory, the display 294, the camera 293, the wireless communication module 260, and the like. The power management module 241 may also be configured to monitor battery capacity, battery cycle times, battery health (leakage, impedance), and other parameters. In other embodiments, the power management module 241 may also be disposed in the processor 210. In other embodiments, the power management module 241 and the charge management module 240 may be disposed in the same device.
The wireless communication function of the terminal may be implemented by an antenna 1, an antenna 2, an antenna 3, a mobile communication module 250, a satellite communication module 251, a wireless communication module 260, a modem processor, a baseband processor, and the like.
The antennas 1, 2, and 3 are used to transmit and receive electromagnetic wave signals. Each antenna in the terminal may be used to cover a single or multiple communication bands. Different antennas may also be multiplexed to improve the utilization of the antennas. For example: the antenna 1 may be multiplexed into a diversity antenna of a wireless local area network. In other embodiments, the antenna may be used in conjunction with a tuning switch. The antenna 3 may be used to transmit signals to and/or receive signals from satellites.
The mobile communication module 250 may provide a solution for wireless communication including 2G/3G/4G/5G or the like applied on the terminal. The mobile communication module 250 may include at least one filter, switch, power amplifier, low noise amplifier (low noise amplifier, LNA), etc. The mobile communication module 250 may receive electromagnetic waves from the antenna 1, perform processes such as filtering, amplifying, and the like on the received electromagnetic waves, and transmit the processed electromagnetic waves to the modem processor for demodulation. The mobile communication module 250 can amplify the signal modulated by the modem processor, and convert the signal into electromagnetic waves through the antenna 1 to radiate. In some embodiments, at least some of the functional modules of the mobile communication module 250 may be disposed in the processor 210. In some embodiments, at least some of the functional modules of the mobile communication module 250 may be provided in the same device as at least some of the modules of the processor 210.
The satellite communication module 251 may provide a solution for communicating with satellites as applied on a terminal. The satellite communication module 251 may be one or more devices integrating at least one communication processing module. The satellite communication module 251 receives electromagnetic waves via the antenna 3, modulates the electromagnetic wave signals, filters the electromagnetic wave signals, and transmits the processed signals to the processor 210. The satellite communication module 251 may also receive a signal to be transmitted from the processor 210, frequency modulate it, amplify it, and convert it into electromagnetic waves to radiate through the antenna 3.
The modem processor may include a modulator and a demodulator. The modulator is used for modulating the low-frequency baseband signal to be transmitted into a medium-high frequency signal. The demodulator is used for demodulating the received electromagnetic wave signal into a low-frequency baseband signal. The demodulator then transmits the demodulated low frequency baseband signal to the baseband processor for processing. The low frequency baseband signal is processed by the baseband processor and then transferred to the application processor. The application processor outputs sound signals through an audio device (not limited to speaker 270A, receiver 270B, etc.), or displays images or video through display screen 294. In some embodiments, the modem processor may be a stand-alone device. In other embodiments, the modem processor may be provided in the same device as the mobile communication module 250 or other functional module, independent of the processor 210.
The wireless communication module 260 may provide solutions for wireless communication including wireless local area network (wirelesslocal area networks, WLAN) (e.g., wireless fidelity (wireless fidelity, wi-Fi) network), bluetooth (BT), global navigation satellite system (global navigation satellite system, GNSS), frequency modulation (frequency modulation, FM), near field wireless communication technology (near field communication, NFC), infrared technology (IR), etc. for application on a terminal. The wireless communication module 260 may be one or more devices that integrate at least one communication processing module. The wireless communication module 260 receives electromagnetic waves via the antenna 2, modulates the electromagnetic wave signals, filters the electromagnetic wave signals, and transmits the processed signals to the processor 210. The wireless communication module 260 may also receive a signal to be transmitted from the processor 210, frequency modulate it, amplify it, and convert it to electromagnetic waves for radiation via the antenna 2.
In some embodiments, the terminal's antenna 1 is coupled to the mobile communication module 250 and the antenna 2 is coupled to the wireless communication module 260 so that the terminal can communicate with the network and other devices through wireless communication techniques. The wireless communication techniques may include the Global System for Mobile communications (global system for mobile communications, GSM), general packet radio service (general packet radio service, GPRS), code division multiple access (codedivision multiple access, CDMA), wideband code division multiple access (wideband code division multipleaccess, WCDMA), time division code division multiple access (time-division code division multiple access, TDSCDMA), long term evolution (long term evolution, LTE), BT, GNSS, WLAN, NFC, FM, and/or IR techniques, among others. The GNSS may include a global satellite positioning system (global positioning system, GPS), a global navigation satellite system (global navigation satellite system, GLONASS), a beidou satellite navigation system (beidounavigation satellite system, BDS), a quasi zenith satellite system (quasi-zenith satellitesystem, QZSS) and/or a satellite based augmentation system (satellite based augmentation systems, SBAS).
The terminal implements display functions through the GPU, the display screen 294, and the application processor, etc. The GPU is a microprocessor for image processing, and is connected to the display screen 294 and the application processor. The GPU is used to perform mathematical and geometric calculations for graphics rendering. Processor 210 may include one or more GPUs that execute program instructions to generate or change display information.
The display 294 is used to display images, videos, and the like. The display 294 includes a display panel. The display panel may employ a liquid crystal display (liquid crystaldisplay, LCD), an organic light-emitting diode (OLED), an active-matrix organic light emitting diode (AMOLED), a flexible light-emitting diode (flex), a mini, a Micro-OLED, a quantum dot light-emitting diode (quantum dot light emitting diodes, QLED), or the like.
The terminal may implement a photographing function through an ISP, a camera 293, a video codec, a GPU, a display 294, an application processor, and the like.
The ISP is used to process the data fed back by the camera 293. For example, when photographing, the shutter is opened, light is transmitted to the camera photosensitive element through the lens, the optical signal is converted into an electric signal, and the camera photosensitive element transmits the electric signal to the ISP for processing and is converted into an image visible to naked eyes. ISP can also optimize the noise, brightness and skin color of the image. The ISP can also optimize parameters such as exposure, color temperature and the like of a shooting scene. In some embodiments, the ISP may be provided in the camera 293.
The camera 293 is used to capture still images or video. The object generates an optical image through the lens and projects the optical image onto the photosensitive element. The photosensitive element may be a charge coupled device (charge coupled device, CCD) or a Complementary Metal Oxide Semiconductor (CMOS) phototransistor. The photosensitive element converts the optical signal into an electrical signal, which is then transferred to the ISP to be converted into a digital image signal. The ISP outputs the digital image signal to the DSP for processing. The DSP converts the digital image signal into an image signal in a standard RGB, YUV, or the like format. In some embodiments, the terminal may include 1 or N cameras 293, N being a positive integer greater than 1.
The camera 293 may also be used to provide a personalized, scenic business experience to the user based on perceived external circumstances and user actions. The camera 293 can acquire abundant and accurate information, so that the terminal perceives external environment and actions of a user. Specifically, in the embodiment of the present application, the camera 293 may be used to identify whether the user of the terminal is the first user or the second user.
The digital signal processor is used for processing digital signals, and can process other digital signals besides digital image signals. For example, when the terminal selects a frequency bin, the digital signal processor is used to fourier transform the frequency bin energy, etc.
Video codecs are used to compress or decompress digital video. The terminal may support one or more video codecs. In this way, the terminal may play or record video in multiple encoding formats, such as: dynamic picture experts group (moving picture experts group, MPEG) 1, MPEG2, MPEG3, MPEG4, etc.
The NPU is a neural-network (NN) computing processor, and can rapidly process input information by referencing a biological neural network structure, for example, referencing a transmission mode between human brain neurons, and can also continuously perform self-learning. Applications such as intelligent cognition of the terminal can be realized through the NPU, for example: image recognition, face recognition, speech recognition, text understanding, etc.
The external memory interface 220 may be used to connect an external memory card, such as a Micro SD card, to realize the memory capability of the expansion terminal. The external memory card communicates with the processor 210 through an external memory interface 220 to implement data storage functions. For example, files such as music, video, etc. are stored in an external memory card.
Internal memory 221 may be used to store computer executable program code that includes instructions. The processor 210 executes various functional applications of the terminal and data processing by executing instructions stored in the internal memory 221. For example, in an embodiment of the present application, the processor 210 may display corresponding display contents on the display screen in response to a user's operation on the display screen 294 by executing instructions stored in the internal memory 221. The internal memory 221 may include a storage program area and a storage data area. The storage program area may store an application program (such as a sound playing function, an image playing function, etc.) required for at least one function of the operating system, etc. The storage data area may store data (e.g., audio data, phonebook, etc.) created during use of the terminal, etc. In addition, the internal memory 221 may include a high-speed random access memory, and may further include a nonvolatile memory, such as at least one magnetic disk storage device, a flash memory device, a universal flash memory (UFS), and the like.
The terminal may implement audio functions through an audio module 270, a speaker 270A, a receiver 270B, a microphone 270C, an earphone interface 270D, an application processor, and the like. Such as music playing, recording, etc.
The audio module 270 is used to convert digital audio information into an analog audio signal output and also to convert an analog audio input into a digital audio signal. The audio module 270 may also be used to encode and decode audio signals. In some embodiments, the audio module 270 may be disposed in the processor 210, or some functional modules of the audio module 270 may be disposed in the processor 210. Speaker 270A, also referred to as a "horn," is used to convert audio electrical signals into sound signals. The terminal can listen to music through the speaker 270A or to hands-free conversations. A receiver 270B, also referred to as a "earpiece", is used to convert the audio electrical signal into a sound signal. When the terminal picks up a call or voice message, the voice can be picked up by placing the receiver 270B close to the human ear. Microphone 270C, also referred to as a "microphone" or "microphone," is used to convert sound signals into electrical signals. When making a call or sending a voice message or when it is desired to trigger the terminal to perform certain functions by means of a voice assistant, the user can sound near the microphone 270C through his mouth, inputting a sound signal to the microphone 270C. The terminal may be provided with at least one microphone 270C. In other embodiments, the terminal may be provided with two microphones 270C, and may implement a noise reduction function in addition to collecting sound signals. In other embodiments, the terminal may be further provided with three, four or more microphones 270C to collect sound signals, reduce noise, identify the source of sound, implement directional recording functions, etc.
The earphone interface 270D is for connecting a wired earphone. Earphone interface 270D may be USB interface 230 or a 3.5mm open mobile terminal platform (open mobile terminal platform, OMTP) standard interface, american cellular telecommunications industry association (cellular telecommunications industry association of the USA, CTIA) standard interface.
The pressure sensor 280A is used to sense a pressure signal, and may convert the pressure signal into an electrical signal. In some embodiments, pressure sensor 280A may be disposed on display 294. The pressure sensor 280A is of various types, such as a resistive pressure sensor, an inductive pressure sensor, a capacitive pressure sensor, and the like. The capacitive pressure sensor may be a capacitive pressure sensor comprising at least two parallel plates with conductive material. When a force is applied to the pressure sensor 280A, the capacitance between the electrodes changes. The terminal determines the strength of the pressure from the change in capacitance. When a touch operation is applied to the display 294, the terminal detects the intensity of the touch operation according to the pressure sensor 280A. The terminal may also calculate the location of the touch based on the detection signal of the pressure sensor 280A. In some embodiments, touch operations that act on the same touch location, but at different touch operation strengths, may correspond to different operation instructions. For example: when a touch operation with the touch operation intensity smaller than the pressure threshold is applied to the short message application icon, executing an instruction for checking the short message. And executing the instruction of newly creating the short message when the touch operation with the touch operation intensity being larger than or equal to the pressure threshold acts on the short message application icon.
The gyro sensor 280B may be used to determine a motion gesture of the terminal. In some embodiments, the angular velocity of the terminal about three axes (i.e., x, y, and z axes) may be determined by gyro sensor 280B. The gyro sensor 280B may be used for photographing anti-shake. Illustratively, when the shutter is pressed, the gyro sensor 280B detects the shake angle of the terminal, calculates the distance to be compensated by the lens module according to the angle, and makes the lens counteract the shake of the terminal through the reverse movement, thereby realizing the anti-shake. The gyro sensor 280B may also be used for navigating, somatosensory game scenes. In addition, the gyro sensor 280B may also be used to measure a rotation amplitude or a moving distance of the terminal.
The air pressure sensor 280C is used to measure air pressure. In some embodiments, the terminal calculates altitude from barometric pressure values measured by barometric pressure sensor 280C, aiding in positioning and navigation.
The magnetic sensor 280D includes a hall sensor. The terminal can detect the opening and closing of the flip holster using the magnetic sensor 280D. In some embodiments, when the terminal is a flip machine, the terminal may detect the opening and closing of the flip according to the magnetic sensor 280D. And then according to the detected opening and closing state of the leather sheath or the opening and closing state of the flip, the characteristics of automatic unlocking of the flip and the like are set.
The acceleration sensor 280E may detect the magnitude of the acceleration of the terminal in various directions (typically three axes). The magnitude and direction of gravity can be detected when the terminal is stationary. The method can also be used for identifying the gesture of the terminal, and is applied to the applications such as horizontal and vertical screen switching, pedometers and the like. In addition, the acceleration sensor 280E may also be used to measure the orientation of the terminal (i.e., the directional vector of the orientation).
A distance sensor 280F for measuring distance. The terminal may measure the distance by infrared or laser. In some embodiments, the terminal may range using the distance sensor 280F to achieve fast focusing to capture a scene.
Proximity light sensor 280G may include, for example, a Light Emitting Diode (LED) and a light detector, such as a photodiode. The light emitting diode may be an infrared light emitting diode. The terminal emits infrared light outwards through the light emitting diode. The terminal uses a photodiode to detect infrared reflected light from nearby objects. When sufficient reflected light is detected, it can be determined that there is an object near the terminal. When insufficient reflected light is detected, the terminal may determine that there is no object in the vicinity of the terminal. The terminal can detect that the user holds the terminal close to the ear by using the proximity light sensor 280G so as to automatically extinguish the screen to achieve the purpose of saving electricity. The proximity light sensor 280G may also be used in holster mode, pocket mode to automatically unlock and lock the screen.
The ambient light sensor 280L is used to sense ambient light level. The terminal may adaptively adjust the brightness of the display 294 according to the perceived ambient light level. The ambient light sensor 280L may also be used to automatically adjust white balance during photographing. The ambient light sensor 280L may also cooperate with the proximity light sensor 280G to detect if the terminal is in a pocket to prevent false touches.
The fingerprint sensor 280H is used to collect a fingerprint. The terminal can utilize the fingerprint characteristic of gathering to realize fingerprint unblock, visit application lock, fingerprint is photographed, fingerprint answer incoming call etc..
The temperature sensor 280J is used to detect temperature. In some embodiments, the terminal performs a temperature processing strategy using the temperature detected by temperature sensor 280J. For example, when the temperature reported by the temperature sensor 280J exceeds a threshold, the terminal performs a reduction in the performance of a processor located near the temperature sensor 280J in order to reduce power consumption for thermal protection. In other embodiments, the terminal heats the battery 242 when the temperature is below another threshold to avoid the terminal from being abnormally shut down due to low temperatures. In other embodiments, when the temperature is below a further threshold, the terminal performs boosting of the output voltage of the battery 242 to avoid abnormal shutdown caused by low temperatures.
The touch sensor 280K, also referred to as a "touch panel". The touch sensor 280K may be disposed on the display screen 294, and the touch sensor 280K and the display screen 294 form a touch screen, which is also referred to as a "touch screen". The touch sensor 280K is used to detect a touch operation acting on or near it. The touch sensor may communicate the detected touch operation to the application processor to determine the touch event type. Visual output related to touch operations may be provided through the display 294. In other embodiments, the touch sensor 280K may also be disposed on a surface of the terminal at a different location than the display 294.
Bone conduction sensor 280M may acquire a vibration signal. In some embodiments, bone conduction sensor 280M may acquire a vibration signal of a human vocal tract vibrating bone pieces. The bone conduction sensor 280M may also contact the pulse of the human body to receive the blood pressure pulsation signal. In some embodiments, bone conduction sensor 280M may also be provided in a headset, in combination with an osteoinductive headset. The audio module 270 may analyze the voice signal based on the vibration signal of the sound portion vibration bone piece obtained by the bone conduction sensor 280M, so as to implement the voice function. The application processor can analyze heart rate information based on the blood pressure beat signal acquired by the bone conduction sensor 280M, so as to realize a heart rate detection function.
The motion sensor 280N may acquire motion data.
Keys 290 include a power on key, a volume key, etc. The keys 290 may be mechanical keys. Or may be a touch key. The terminal may receive key inputs, generating key signal inputs related to user settings of the terminal as well as function controls.
The terminal recognizes the operations (including the first operation, the second operation, the third operation, etc.) mentioned in the embodiment of the present application through various sensors in the sensor module 280, the key 290, and/or the camera 293.
The motor 291 may generate a vibration alert. The motor 291 may be used for incoming call vibration alerting or for touch vibration feedback. For example, touch operations acting on different applications (e.g., photographing, audio playing, etc.) may correspond to different vibration feedback effects. The motor 291 may also correspond to different vibration feedback effects by touch operations applied to different areas of the display 294. Different application scenarios (such as time reminding, receiving information, alarm clock, game, etc.) can also correspond to different vibration feedback effects. The touch vibration feedback effect may also support customization.
The indicator 292 may be an indicator light, which may be used to indicate a state of charge, a change in power, a message indicating a missed call, a notification, etc.
The SIM card interface 295 is for interfacing with a SIM card. The SIM card may be inserted into the SIM card interface 295 or removed from the SIM card interface 295 to enable contact and separation from the terminal. The terminal may support 1 or N SIM card interfaces, N being a positive integer greater than 1. The SIM card interface 295 may support Nano SIM cards, micro SIM cards, and the like. The same SIM card interface 295 may be used to insert multiple cards simultaneously. The types of the plurality of cards may be the same or different. The SIM card interface 295 may also be compatible with different types of SIM cards. The SIM card interface 295 may also be compatible with external memory cards. The terminal interacts with the network through the SIM card to realize the functions of communication, data communication and the like. In some embodiments, the terminal employs esims, i.e.: an embedded SIM card. The eSIM card can be embedded in the terminal and cannot be separated from the terminal.
The following description will be given of a method for sending and a method for receiving a satellite short message of a terminal according to an embodiment of the present application, taking a mobile phone as an example. The method may be performed by a terminal or by a component of a terminal (e.g., a processor, chip, or system-on-a-chip, etc.).
The method for transmitting the message provided by the embodiment of the application can be applied to the terminal described above, and the method for transmitting the message can comprise a method for transmitting the message and a method for receiving the message, which are respectively described below.
As shown in fig. 3, an embodiment of a method for sending a message according to an embodiment of the present application may include:
301. and the terminal displays a star finding guiding interface.
The satellite finding guiding interface comprises a satellite identifier, and the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relation between the terminal and the target satellite.
In the embodiment of the application, the terminal can respond to the operation of newly building the satellite message or the operation of replying the satellite message by the user, and a satellite message editing interface is displayed and used for inputting the content of the first satellite message by the user. Then, the terminal may display a star finding guidance interface in response to a user's transmission operation of the first satellite message.
In the embodiment of the application, the operations related to the satellite message (such as the operations of newly creating the satellite message or replying to the satellite message) can be completed in the satellite message function item, and the satellite message function item can be set in the information application, for example: short message applications or other communication applications. Of course, a satellite message application may also be designed for satellite messages to implement the functionality of the satellite message function item. If the satellite message function item is set in the short message application, the short message application has the function of a common short message and the function of a satellite short message. If the satellite message function item is set in the instant messaging application, the instant messaging application has an instant messaging function+a satellite message function. If a satellite message application is designed for satellite messages, the satellite message application has at least the functionality of satellite messages.
The user may typically use the functionality of satellite messaging in the event that the signal is poor or mobile communications are out of service. In the embodiment of the present application, the setting is described by taking the short message application as an example, and the satellite message related to the short message application may be called a satellite short message.
Taking a short message application as an example, as shown in fig. 4A, the terminal responds to a click operation of an information application (short message application) 401 on a mobile phone main interface by a user, and displays an information interface as shown in fig. 4B. The information interface includes a satellite short message function item 402. The terminal displays a satellite short message interface as shown in fig. 4C in response to a clicking operation of the satellite short message function item 402 by the user on the information interface shown in fig. 4B. The satellite short message interface includes an identifier 403 of "new satellite short message" and may also include an identifier 404 of "receive satellite short message". The user can enter the interface for receiving the satellite short message through the identifier 403 of the "new satellite short message" and can enter the interface for receiving the satellite short message through the identifier 404 of the "receiving satellite short message". It should be noted that, the scenario listed in the embodiment of the present application is illustrated by taking a short message as an example, and if the scenario is not a short message scenario, the word pattern of the satellite short message in fig. 4B and fig. 4C may be modified into a satellite message.
In the process of transmitting a satellite message (satellite short message), the terminal responds to the click operation of the user on the identifier 403 of the "new satellite short message", and displays a new satellite short message interface as shown in fig. 4D. The user in the newly created satellite short message interface may select a recipient in the recipient's box, such as recipient "Mary" shown in FIG. 4D, and then edit the content of the first satellite message in the edit box, such as "everything is normal, do not worry" shown in FIG. 4D. The short message interface of the newly-built satellite provided by the embodiment of the application can include a mark 405 carrying the position, the mark is usually in a default selection state, and the terminal can automatically carry the position information of the position where the current terminal is located when sending the content of the first satellite message to the target satellite. Of course, the user can cancel the function of carrying the position by clicking on the position of "/". If the function of carrying the position is not checked, the position information of the position where the current terminal is located is not carried when the content of the first satellite message is sent.
In the embodiment of the present application, the terminal may display the loading interface as shown in fig. 5A in response to the clicking operation of the send button 406 in fig. 4D by the user. The loading interface can display prompt information such as "please be in open area as much as possible, avoid foreign matter shielding signal on sight space", and also can display loading progress.
It should be noted that, in response to the clicking operation of the send button 406 by the user, the terminal may not display the loading interface as shown in fig. 5A, may directly display the loaded result interface, and the loaded result interface may be referred to as the star finding guiding interface.
302. And the terminal responds to the mobile operation of the user on the terminal and updates the display position of the satellite identifier.
In the embodiment of the application, the star finding guiding interface is used for guiding the user to adjust the position of the terminal. The user can determine the position relationship between the terminal and the target satellite through the display position of the satellite identifier in the satellite searching guide interface, and then the mobile terminal (such as a leftward or rightward mobile terminal and an upward or downward mobile terminal) responds to the movement to adjust the display position of the satellite identifier on the satellite searching guide interface.
303. And if the position relation between the mobile terminal and the target satellite meets the message transmission condition, the terminal sends a first satellite message to the target satellite.
In the embodiment of the application, the condition that the position relationship between the mobile terminal and the target satellite satisfies the message transmission condition may be that the position relationship between the mobile terminal and the target satellite enables the terminal to establish communication connection with the target satellite.
In the embodiment of the application, the terminal can guide the user to adjust the position relationship between the terminal and the target satellite through the satellite finding guiding interface, so that the terminal can quickly establish communication connection with the satellite, and the terminal can quickly send satellite information.
In the embodiment of the application, the star finding guiding interface can also comprise star finding prompting information, and the star finding prompting information is used for prompting the direction of the mobile terminal of the user. If the satellite finding prompt information is a leftward mobile terminal, a rightward mobile terminal, an upward mobile terminal or a downward mobile terminal. It should be noted that, the satellite finding prompt information is usually a prompt given by the terminal according to the shortest moving path, so that the user can move the terminal to a position suitable for establishing communication connection with the target satellite according to the satellite finding prompt information, thereby accelerating the speed of the terminal sending satellite information to the target satellite or receiving satellite information.
The satellite finding guiding interface and the interface for sending satellite messages in the embodiment of the application can have various expression forms, and the expression forms are related to the sequence of adjusting the azimuth angle and the pitch angle of the terminal and the target satellite. As for the azimuth angle and the pitch angle, the three-dimensional coordinate system (xyz) shown in fig. 5B can be referred to, as shown in fig. 5B, the terminal is located at the center of the three-dimensional coordinate system, the antenna on the terminal for communicating with the satellite is in the y-axis direction, then the azimuth angle is the included angle between the y-axis and the line connecting the projection point C of the satellite on the xy-plane with the center of the circle, and the pitch angle is the included angle between the projection point C of the satellite on the xy-plane with the center of the circle and the line connecting the satellite with the center of the circle.
In the embodiment of the application, the star finding guiding interface can comprise a first star finding guiding interface and a second star finding guiding interface. The first satellite searching guide interface comprises a first satellite identifier and a first alignment area, wherein the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in azimuth, and when the position relation between the terminal and the target satellite in azimuth meets the message transmission condition, the first satellite identifier is located in the first alignment area. The second satellite searching guide interface comprises a second satellite identifier and a second alignment area, wherein the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is positioned in the second alignment area.
In the embodiment of the application, the star finding guiding interface is not divided into a first star finding guiding interface and a second star finding guiding interface, but the star finding guiding interface comprises a first satellite identifier and a first alignment area, and a second satellite identifier and a second alignment area; the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and is positioned in the first alignment area when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition; the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is located in the second alignment area.
In the embodiment of the application, the expression forms of the satellite finding guiding interfaces are related to the sequence of adjusting the azimuth angle and the pitch angle of the terminal and the target satellite, and the satellite finding guiding interfaces with different expression forms are introduced according to the sequence of adjusting the azimuth angle and the pitch angle of the terminal and the target satellite.
Scheme 1. A star finder interface (first star finder interface) for azimuth adjustment.
In the embodiment of the present application, a star finding guiding interface in adjusting the azimuth angle can be understood by referring to fig. 5C. As shown in fig. 5C, the information 501 of "in the satellite searching" is displayed in the satellite searching guiding interface, and the identifier 502 of "signal state" is also displayed, so in fig. 5C, all four signal grids are in blank state, which indicates that no signal is yet present, the area for adjusting the position relationship between the terminal and the target satellite in fig. 5C is represented by a circular disc area 503, the first satellite identifier 504 is displayed in the circular disc area 503, the area covered by the antenna for communicating with the target satellite is represented by a sector, which is generally a range of plus or minus 15 ° of the center line of the circular disc area 503, the center line is a line crossing the center of the circular disc 503 and parallel to the y axis, and the sector area may be referred to as a first alignment area 505. The star finding guidance interface may also display a star finding prompt message, such as the word 506 of "turn mobile phone to the right" in fig. 5C, which is a star finding prompt message for adjusting azimuth angle.
It should be noted that, in the embodiment of the present application, the positions of the first satellite identifier 504 and the first alignment area 505 in the circular area 505 are determined by using the position of the antenna in the terminal for communicating with the target satellite as a reference, and the horizontal position of the target satellite relative to the terminal is determined, and the first satellite identifier 504 is displayed in the corresponding position of the circular area 503. The location of the first satellite identification 504 may be determined by reverse calculation by way of cell phone positioning by the target satellite.
It should be noted that, the specific content of the satellite finding prompt information displayed on the satellite finding guiding interface is related to the position where the first satellite identifier 504 is located, as in fig. 5C, where the first satellite identifier 504 is located on the right side of the first alignment area 505, that is, in a range from 0 ° to 180 ° on the right side of the center line of the first alignment area 505, so that, in order to enable the first satellite identifier 504 to enter the first alignment area 505 with a shorter path or with a smaller rotation angle, the terminal will generally give the satellite finding prompt information of "turning the mobile phone right". If the first satellite tag 504 is located on the left side of the first alignment area 505, i.e., in the range of 0 ° to 180 ° from the left side of the center line of the first alignment area 505, the terminal will typically give a "turn left" star finding hint to the mobile phone in order to allow the first satellite tag 504 to enter the first alignment area 505 with a shorter path or with a smaller angle of rotation. Although in the embodiment of the present application, a schematic view of the first satellite identifier 504 being located on the left side of the first alignment area 505 is not given, it is also easy to understand, in connection with fig. 5C, that the first satellite identifier 504 is located on the left side of the first alignment area 505 according to the text description herein.
On the star-finding guidance interface shown in fig. 5C, if the user operates according to the star-finding prompt information of "turn mobile phone to the right", or if the user turns the mobile phone to the left by 360 ° and the difference between the degrees of turn to the right, the first satellite identifier 504 can be turned to the first alignment area 505, and the interface of the terminal will be refreshed accordingly, so as to display the star-finding guidance interface shown in fig. 5D. In the star-finding guidance interface shown in fig. 5D, the first satellite identifier 504 is located at the position of the center line of the first alignment area 505, which indicates that the azimuth angle is adjusted, and because the pitch angle is not yet adjusted, all four signal cells of the identifier 502 of "signal state" in the star-finding guidance interface shown in fig. 5D are still in a blank state.
It should be noted that, in the embodiment of the present application, when the display position of the first satellite identifier is located outside the first alignment area, the first alignment area is displayed with a first color; when the display position of the first satellite mark is positioned in the first alignment area, the first alignment area is displayed in a second color, and the first color is different from the second color.
In combination with the foregoing satellite short message scenario, with respect to fig. 5C, the first alignment area 505 may be displayed in a first color when the azimuth has not been adjusted, as shown in fig. 5E, and after the azimuth has been adjusted, the first satellite identifier 504 is located in the first alignment area 505, with respect to fig. 5D, the first alignment area 505 may be displayed in a second color, as shown in fig. 5F, where the first color is different from the second color. In this way, the user can be better prompted by the color change that the azimuth alignment has been completed.
Scheme 2. A star finder interface (second star finder interface) for adjusting pitch angle.
In the embodiment of the present application, a star-finding guiding interface in adjusting a pitch angle can be understood by referring to fig. 6A. As shown in fig. 6A, the information of "in the satellite searching" is displayed in the satellite searching guiding interface, and the identifier of "signal state" is also displayed, so that in fig. 6A, four signal cells are all in a blank state, which indicates that no signal is yet present, and the area for adjusting the positional relationship between the terminal and the target satellite in fig. 6A is represented by a disc area. The description of 501, 502, and 503 may be understood with reference to fig. 5C with respect to these items in fig. 6A.
A second satellite identification 601 is shown in the carousel area and the second alignment area 602 is a small carousel in communication with the carousel area. The star finding guiding interface can also display a star finding prompt message, such as a word 603 of "up-lifting mobile phone" in fig. 6A, which is a star finding prompt message for adjusting pitch angle.
It should be noted that, in the embodiment of the present application, the positions of the second satellite identifier 601 and the second alignment area 602 in the circular area are determined by using the position of the antenna in the terminal, which communicates with the target satellite, as a reference, and the pitch position of the target satellite relative to the terminal, and the second satellite identifier 601 is displayed in the corresponding position in the circular area.
It should be noted that, the specific content of the satellite finding prompt information displayed on the satellite finding guiding interface is related to the position of the second satellite identifier 601, as in fig. 6A, the second satellite identifier 601 is located under the second alignment area 602, and the terminal will give the satellite finding prompt information of "lifting the mobile phone upwards". If the second satellite identifier 601 is located directly above the second alignment area 602, the terminal will give a "push down handset" star finding prompt. Although in the embodiment of the present application, a schematic view of the second satellite identifier 601 being located directly above the second alignment area 602 is not given, the solution that the second satellite identifier 601 is located directly above the second alignment area 602 is also easily understood in connection with fig. 6A according to the text description herein.
On the star-finding guidance interface shown in fig. 6A, if the user operates according to the star-finding prompt information of "lift up the mobile phone", the second satellite identifier 601 is moved to the second alignment area 602, and the interface of the terminal is refreshed accordingly, so that the star-finding guidance interface shown in fig. 6B is displayed. In the star-finding guidance interface shown in fig. 6B, the second satellite identifier 601 is located at the center of the second alignment area 602, which indicates that the pitch angle has been adjusted.
It should be noted that, when the display position of the second satellite identifier is located outside the second alignment area, the second alignment area is displayed with a third color; when the display position of the second satellite mark is positioned in the second alignment area, the second alignment area is displayed in a fourth color, and the third color is different from the fourth color.
In combination with the foregoing satellite short message scenario, with respect to fig. 6A, the second alignment area 602 may be displayed in a third color when the azimuth is not yet adjusted, and after the azimuth is adjusted, the second satellite identifier 601 is located in the second alignment area 602, and the second alignment area 602 may be further displayed in a fourth color, where the third color is different from the fourth color, and although the color change process of the second alignment area 602 is not illustrated by a schematic diagram, it can also be understood in combination with the color change process of fig. 5E and 5F. In this way, the user can be better prompted through the color change that the alignment of the pitch angle is completed.
And 3. A star finding guiding interface for firstly adjusting azimuth angle and then adjusting pitch angle.
The scheme 3 displays a first star-finding guiding interface and then displays a second star-finding guiding interface, corresponding to the previous steps 301 and 302, and the process specifically may include: displaying a first satellite finding guiding interface, and updating the display position of a first satellite identifier in response to the leftward movement operation or the rightward movement operation of a user on the terminal; displaying a second satellite finding guiding interface when the first satellite identifier is positioned in the first alignment area; and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
In combination with the satellite short message scenario described in the foregoing schemes 1 and 2, in the embodiment of the present application, if the satellite finding adjustment is performed according to the order of adjusting the azimuth angle and then adjusting the pitch angle, the terminal displays fig. 5C, fig. 5D, fig. 6A and fig. 6B sequentially, and then an interface for sending the satellite message as shown in fig. 6C may be obtained. As shown in fig. 6C, the second satellite identification 601 and the second alignment area 602 of the interface for adjusting the pitch angle may be displayed only at the interface for transmitting the satellite short message, and the first satellite identification 504 and the first alignment area 505 may not be displayed, according to the order of azimuth-first and pitch angle. In addition, 3 of the four-cell signals in the "signal state" identifier 604 on the interface for transmitting satellite short messages are in a full-cell state, which indicates that a connection has been established with a satellite, and the "transmitting" word 605 and the "please hold a hand gesture" word 606 may also be displayed on the interface for transmitting satellite short messages.
Scheme 4. A star finding guiding interface for adjusting pitch angle and azimuth angle.
The solution 4 displays the second star finding guiding interface first and then displays the first star finding guiding interface, which corresponds to the previous steps 301 and 302, and the process specifically may include: displaying a second satellite finding guiding interface, and updating the display position of a second satellite identifier in response to the upward movement operation or the downward movement operation of a user on the terminal; displaying a first satellite finding guiding interface when the second satellite identifier is positioned in the second alignment area; and updating the display position of the first satellite identifier in response to the leftward or rightward movement operation of the terminal by the user.
In combination with the satellite short message scenario described in the foregoing schemes 1 and 2, in the embodiment of the present application, if the satellite finding adjustment is performed according to the order of adjusting the pitch angle and then adjusting the azimuth angle, the terminal displays fig. 6A, fig. 6B, fig. 5C, and fig. 5D sequentially, and then an interface for sending the satellite short message as shown in fig. 6D may be obtained. As shown in fig. 6D, the first satellite identification 504 and the first alignment area 505 of the interface for adjusting the azimuth may be displayed only at the interface for transmitting the satellite short message, and the second satellite identification 601 and the second alignment area 602 may not be displayed, according to the order of pitch angle and then azimuth. In addition, 3 of the four-cell signals in the "signal state" identifier 604 on the interface for transmitting satellite short messages are in a full-cell state, which indicates that a connection has been established with a satellite, and the "transmitting" word 605 and the "please hold a hand gesture" word 606 may also be displayed on the interface for transmitting satellite short messages.
And 5, another star finding guiding interface for firstly adjusting azimuth angle and then adjusting pitch angle.
In the scheme 5, a first satellite finding guiding interface is displayed firstly, then a second satellite finding guiding interface is displayed, and the second satellite finding guiding interface which is different from the part of the scheme 3 does not display the first satellite identification and the first alignment area is that: the second satellite finding guidance interface in this scenario 5 also displays the first satellite identification and the first alignment area.
In combination with the foregoing satellite short message scenario, in the embodiment of the present application, if the star finding adjustment is performed according to the sequence of adjusting the azimuth angle and then adjusting the pitch angle, the terminal displays the star finding guiding interface shown in fig. 5C, fig. 5D, and then fig. 7A.
As shown in fig. 7A, the satellite finding guidance interface displays not only the second satellite identification 601 and the second alignment area 602, but also the first satellite identification 504 and the first alignment area 505 when adjusting the pitch angle. In addition, the star finding guidance interface shown in fig. 7A may also display the words of "star finding prompt information for lifting the mobile phone upwards," signal state, "and" in star finding. For these matters, the foregoing description of fig. 6A has been already described, and the description will not be repeated here.
On the star-finding guidance interface shown in fig. 7A, if the user operates according to the star-finding prompt information of "lift up the mobile phone", the second satellite identifier 601 is moved to the second alignment area 602, and the interface of the terminal is refreshed accordingly, so that the star-finding guidance interface shown in fig. 7B is displayed. In the satellite-finding guidance interface shown in fig. 7B, the second satellite identifier 601 is located at the center of the second alignment area 602, which indicates that the pitch angle has been adjusted, and also indicates that the first satellite identifier 504 is located in the first alignment area 505.
It should be noted that, if the first satellite identifier 504 deviates from the first alignment area 505 during the pitch angle adjustment, the first satellite identifier 504 may be adjusted back to the first alignment area 505 again by using the principle of azimuth angle adjustment described above.
Based on fig. 7B, the terminal refreshes the interface for sending satellite short message as shown in fig. 7C. As shown in fig. 7C, the second satellite identifier 601 and the second alignment area 602 of the interface for adjusting the pitch angle and the first satellite identifier 504 and the first alignment area 505 may be displayed on the interface for transmitting the satellite short message according to the sequential adjustment of the azimuth angle and the pitch angle. In addition, 3 of the four-cell signals in the "signal state" identifier 604 on the interface for transmitting satellite short messages are in a full-cell state, which indicates that a connection has been established with a satellite, and the "transmitting" word 605 and the "please hold a hand gesture" word 606 may also be displayed on the interface for transmitting satellite short messages.
And 6, another star finding guiding interface for firstly adjusting the pitch angle and then adjusting the azimuth angle.
In the scheme 6, a second satellite finding guiding interface is displayed firstly, then a first satellite finding guiding interface is displayed, and the first satellite finding guiding interface which is different from the part of the scheme 4 does not display a second satellite identifier and a second alignment area is that: the first satellite finding guidance interface of this aspect 6 also displays a second satellite identification and a second alignment area.
In combination with the foregoing satellite short message scenario, in the embodiment of the present application, if the star finding adjustment is performed according to the order of adjusting the pitch angle and then adjusting the azimuth angle, the terminal displays the star finding guidance interface shown in fig. 6A and fig. 6B, and then displays the star finding guidance interface shown in fig. 8A.
As shown in fig. 8A, the satellite finding guidance interface displays not only the first satellite identification 504 and the first alignment area 505 but also the second satellite identification 601 and the second alignment area 602 when adjusting the pitch angle. In addition, the star finding guidance interface shown in fig. 8A may also display the words of "star finding prompt information of" turn mobile phone to the right, "signal state," and "in star finding. For these matters, the foregoing description of fig. 5C has been already described, and the description will not be repeated here.
On the star-finding guidance interface shown in fig. 8A, if the user operates according to the star-finding prompt information of "turn mobile phone to the right", the first satellite identifier 504 is turned to the first alignment area 505, and the interface of the terminal is refreshed accordingly, so that the star-finding guidance interface shown in fig. 7B is displayed. In the satellite-finding guidance interface shown in fig. 7B, the first satellite identifier 504 is located in the first alignment area 505, which indicates that the azimuth angle has been adjusted, and the second satellite identifier 601 is also displayed in the second alignment area 602.
It should be noted that, if the second satellite identifier 601 deviates from the second alignment area 602 during the azimuth adjustment, the second satellite identifier 601 may be adjusted back to the second alignment area 602 again by using the principle of adjusting the pitch angle as described above.
Based on fig. 7B, the terminal refreshes the interface for sending satellite short message as shown in fig. 7C. As shown in fig. 7C, the first satellite identifier 504 and the first alignment area 505 of the interface for adjusting the azimuth angle and the second satellite identifier 601 and the second alignment area 602 may be displayed on the interface for transmitting the satellite short message according to the order of pitch angle and then azimuth angle. In addition, 3 of the four-cell signals in the "signal state" identifier 604 on the interface for transmitting satellite short messages are in a full-cell state, which indicates that a connection has been established with a satellite, and the "transmitting" word 605 and the "please hold a hand gesture" word 606 may also be displayed on the interface for transmitting satellite short messages.
And 7, another star finding guiding interface for firstly adjusting azimuth angle and then adjusting pitch angle.
The satellite-finding guidance interface of aspect 7 includes a first satellite identification and a first alignment area, and a second satellite identification and a second alignment area. Step 302 in the previous embodiment specifically includes: responding to the leftward movement operation or rightward movement operation of the user on the terminal, and updating the display position of the first satellite identifier; and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
In combination with the foregoing satellite short message scenario, in the embodiment of the present application, if the star finding adjustment is performed according to the sequence of adjusting the azimuth angle and then adjusting the pitch angle, the terminal may display the star finding guiding interface as shown in fig. 8B in sequence.
As shown in fig. 8B, in the satellite finding guiding interface, not only the first satellite identification 504 and the first alignment area 505, but also the second satellite identification 601 and the second alignment area 602 are displayed when the azimuth is adjusted. In addition, the star finding guidance interface shown in fig. 8B may also display the words of "star finding prompt information of" turn mobile phone to the right, "signal state," and "in star finding. For these matters, the foregoing description of fig. 5C has been already described, and the description will not be repeated here.
On the star-finding guidance interface shown in fig. 8B, if the user operates according to the star-finding prompt information of "turn mobile phone to the right", the first satellite identifier 504 is turned to the first alignment area 505, and the interface of the terminal is refreshed accordingly, so that the star-finding guidance interface shown in fig. 7A is displayed. Then, the pitch angle is adjusted on the basis of the star finding guiding interface shown in fig. 7A to refresh the star finding guiding interface shown in fig. 7B, and then the interface for sending satellite short messages shown in fig. 7C is refreshed.
Scheme 8. Another star-finding guidance interface that adjusts pitch angle first and then azimuth angle.
In combination with the foregoing satellite short message scenario, in the embodiment of the present application, if the star finding adjustment is performed according to the order of adjusting the pitch angle and then adjusting the azimuth angle, the terminal may display the star finding guiding interface as shown in fig. 8C in order.
As shown in fig. 8C, in the satellite finding guiding interface, not only the first satellite identification 504 and the first alignment area 505, but also the second satellite identification 601 and the second alignment area 602 are displayed when the azimuth is adjusted. In addition, the star finding guidance interface shown in fig. 8C may also display the words of "up-mobile" such as "signal status" and "in star finding". For these matters, the foregoing description of fig. 5C has been already described, and the description will not be repeated here.
On the star-finding guidance interface shown in fig. 8C, if the user operates according to the star-finding prompt information of "lift up the mobile phone", the second satellite identifier 601 is moved to the second alignment area 602, and the interface of the terminal is refreshed accordingly, so that the star-finding guidance interface shown in fig. 8A is displayed. Then, the azimuth angle is adjusted on the basis of the star finding guiding interface shown in fig. 8A to refresh the star finding guiding interface shown in fig. 7B, and then the interface for sending satellite short messages shown in fig. 7C is refreshed.
Scheme 9. A star-finding guidance interface for adjusting azimuth and pitch angles simultaneously.
In combination with the foregoing satellite short message scenario, in the embodiment of the present application, not only azimuth angle and pitch angle may be sequentially adjusted according to the foregoing 8 schemes, but also azimuth angle and pitch angle may be simultaneously adjusted, when the azimuth angle pitch angle is simultaneously adjusted, the terminal may directly display a star finding guiding interface as shown in fig. 9, and in fig. 9, unlike in fig. 8B or fig. 8C, the star finding prompting message in fig. 9 is "turn mobile phone right+lift mobile phone upward".
On the star-finding guiding interface shown in fig. 9, if the user synchronously operates according to the star-finding prompt information of "turn mobile phone right and lift mobile phone up", the first satellite identifier 504 is turned to the first alignment area 505, the second satellite identifier 601 is moved to the second alignment area 602, and the interface of the terminal is refreshed accordingly, so that the star-finding guiding interface shown in fig. 7B is displayed, and the interface for sending satellite short messages shown in fig. 7C is refreshed.
In the above-described scheme for satellite finding adjustment, only the satellite identifier of one satellite is displayed in the satellite finding guiding interface and the interface for sending satellite short messages, in fact, the number of satellites displayed in the satellite finding guiding interface and the interface for sending satellite short messages is not limited in the application, when there are a plurality of satellites capable of communicating with the terminal, the satellite identifiers of a plurality of satellites can be displayed in the satellite finding guiding interface and the interface for sending satellite short messages, and scheme 10 is described below by taking the satellite identifiers of two satellites as an example in combination with scheme 7 when one satellite is displayed in the foregoing.
And 10, displaying a satellite finding guiding interface for firstly adjusting azimuth angles and then adjusting pitch angles when satellite identifications of a plurality of satellites are displayed.
The satellite searching guide interface shown in fig. 10A includes satellite identifiers of two satellites, where a first satellite identifier 504 of a first satellite (target satellite) and a second satellite identifier 601 have been described above, the first satellite identifier of the second satellite is denoted by 1001, and the second satellite identifier is denoted by 1002. In the scheme shown in fig. 10A, it is preferable to adjust the first satellite represented by the first satellite identifier 504, so that the terminal gives a star finding prompt message of "turning the mobile phone to the right" on the star finding guiding interface shown in fig. 10A.
On the basis of fig. 10A, if the user synchronously operates according to the star finding prompt information of "turning the mobile phone to the right", the first satellite identifier 504 is turned to the first alignment area 505, and the interface of the terminal is refreshed accordingly, so that the star finding guiding interface shown in fig. 10B is displayed. The star-finding guiding interface shown in fig. 10B displays the star-finding prompt information of "lift up mobile phone", if the user operates according to the star-finding prompt information of "lift up mobile phone", the second satellite identifier 601 is moved to the second alignment area 602, the interface of the terminal is refreshed accordingly, the star-finding guiding interface shown in fig. 10C is displayed, and the interface for sending satellite short message shown in fig. 10D is refreshed.
In the scheme 10 described in the embodiment of the present application, the first satellite identifier 1001 and the second satellite identifier 1002 of the second satellite are added on the basis of the scheme 7, and in fact, on the basis of the schemes 1-6, 8 and 9 described in the foregoing other schemes than the scheme 7, satellite identifiers of another satellite similar to the one described in the scheme 10 can be added. In addition, the terminal determines the displayed satellite finding prompt information according to the relationship between the other satellite and the first alignment area, so that the satellite finding guiding interface and the satellite short message sending interface of the plurality of satellites can be various, and the embodiment of the application is not described one by one. In addition, in the embodiments of the present application, different colors may be set in the first alignment area and the second alignment area in the schemes 1 to 10 before and after the azimuth angle alignment and the pitch angle alignment, and as can be understood by referring to fig. 5E and fig. 5F, the color filling and changing process will not be described one by one in the embodiments of the present application.
In the embodiment of the present application, after the first satellite message is sent, the method may further include: determining a position change after the terminal transmits the first satellite message in response to a user transmitting operation of the second satellite message; if the position change after the terminal sends the first satellite message is smaller than the first threshold value, the terminal sends the second satellite message to the target satellite, and the satellite finding guiding interface is not displayed.
It may further be that, after the first satellite message is sent, it may further be that: determining a time when the terminal transmits the first satellite message in response to a transmission operation of the user on the second satellite message; if the time difference between the time distance when the terminal sends the first satellite message and the time distance when the user triggers the sending operation of the second satellite message is smaller than a second threshold value, the second satellite message is sent to the target satellite, and the satellite finding guiding interface is not displayed.
In combination with the scenario of the previous satellite short message, in the embodiment of the present application, after the terminal sends the first satellite short message, a message that the satellite feedback is sent successfully may be received, and for the message sent to the recipient "mark" previously, an interface as shown in fig. 11A may be displayed. If the user worry that the second terminal can not successfully receive, the attitude of the terminal with the adjusted azimuth angle and pitch angle can be kept, and the second satellite short message is sent to the same receiver again. Because the time interval between the satellite short message and the last satellite short message transmission is very small or the position change of the mobile phone is very small, the satellite short message can be re-transmitted without entering the satellite searching guide interface again, and if the second satellite short message is also successfully transmitted, the terminal can display the interface shown in fig. 11B.
In the embodiment of the application, after the terminal sends the first satellite short message, the attitude of the terminal with the adjusted azimuth angle and pitch angle can be kept, and the second satellite short message is sent to another receiver, as shown in fig. 11C, and the second satellite short message is sent to the receiver 'Lucy'. Because the time interval between the sending of the second satellite short message to the receiver "Lucy" and the last sending of the satellite short message to the receiver "Mary" is small or the position change of the mobile phone is small, the second satellite short message to the receiver "Lucy" can be sent without entering the satellite searching guiding interface again, and if the sending of the second satellite short message to the receiver "Lucy" is also successful, the terminal will display the interface as shown in FIG. 11D.
Fig. 11A to 11D each depict a case where the satellite short message transmission is successful, and after the first satellite message is transmitted to the target satellite, the method further includes: receiving a response message of failure of the first satellite message transmission; and displaying the star finding guiding interface according to the response message of the failure of the first satellite message transmission.
In combination with the foregoing scenario of satellite short message, when the satellite short message fails to send, for example, the failure to send the second satellite short message to the recipient "Lucy", the terminal will display the interface as shown in FIG. 11E.
Aiming at the situation of failure in transmission, the terminal can display the star finding guiding interface again, so that the user can conveniently perform star finding alignment again. When the transmission fails, the display interface of the terminal can also pop up the prompt message of whether to replace one satellite.
In addition, in the embodiment of the application, the common message which is not successfully sent can be converted into the satellite message to be sent, and the process can be as follows: before displaying the star finding guiding interface, sending a common message to a base station; receiving a response message of failure of sending the common message; and responding to the response message of failure of sending the common message, and displaying a star finding guiding interface.
In the satellite short message scenario, when the transmission of the common short message fails, the terminal may automatically switch to the satellite short message transmission, automatically fill the content of the common short message into the editing area of the satellite short message, and start the satellite searching process described in the previous embodiment. Or, when the sending of the common short message fails, the user is prompted whether to switch to satellite short message sending, if the user selects yes, the user agrees to switch to satellite short message sending, the terminal automatically fills the content of the common short message into the editing area of the satellite short message, and the satellite finding process described in the previous embodiment is started.
The corresponding content of the method of message transmission is described above, and the method of message reception is described below.
As shown in fig. 12, an embodiment of a method for receiving a message according to an embodiment of the present application may include:
1201. and the terminal displays a star finding guiding interface.
The satellite finding guiding interface comprises a satellite identifier, and the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relation between the terminal and the target satellite.
1202. And the terminal responds to the mobile operation of the user on the terminal and updates the display position of the satellite identifier.
1203. And if the position relation between the mobile terminal and the target satellite meets the message transmission condition, the terminal receives the first satellite message from the target satellite.
In the embodiment of the application, the terminal can guide the user to adjust the position relationship between the terminal and the target satellite through the satellite finding guiding interface, so that the terminal can quickly establish communication connection with the satellite, and the terminal can quickly receive satellite information.
In the embodiment of the present application, both steps 1201 and 1202 can be understood by referring to the corresponding contents of the method of receiving the foregoing message. The description will not be repeated here, except that step 1203 receives the first satellite message from the target satellite, and step 303 transmits the first satellite message to the target satellite.
In the embodiment of the present application, taking the satellite message as the satellite short message as an example, the operation of receiving the satellite short message may be performed in the interface shown in fig. 13A, for example, in response to the clicking operation of the user on the identifier 404 of the satellite short message received in fig. 13A, the loading interface shown in fig. 5A is started, or other satellite searching guiding interfaces introduced in the process of receiving the satellite short message are displayed, and then satellite searching guiding is performed according to the schemes 1 to 10 or other possible schemes introduced in the process of receiving the satellite short message, so that the terminal establishes a communication connection with the satellite, and further receives the satellite short message through the satellite.
An interface where the terminal receives the satellite short message can be understood with reference to fig. 13B, as shown in fig. 13B, the satellite short message "start the vehicle to get the position to get me" sent by Peter is received, and the interface also carries the position information.
In the embodiment of the application, the method for transmitting the message and the method for receiving the message can be realized through the satellite, and the alignment of the terminal and the target satellite can be realized, so that the success rate of transmitting the message is improved, especially in the areas where the mobile communication signal is weak or is not served, and the success rate of transmitting the message is improved.
The foregoing describes a process of sending a satellite message and a process of receiving a satellite message, and the following describes a terminal provided by an embodiment of the present application with reference to the accompanying drawings.
As shown in fig. 14, a terminal 140 provided in an embodiment of the present application includes:
and the display unit 1401 is used for displaying a satellite finding guiding interface, wherein the satellite finding guiding interface comprises a satellite identifier, and the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relationship between the terminal and the target satellite.
A processing unit 1402 for updating the display position of the satellite identification displayed by the display unit 1401 in response to a user's movement operation of the terminal.
The transceiver 1403 is configured to send the first satellite message to the target satellite or receive the first satellite message from the target satellite if the processing unit 1402 meets the message transmission condition in response to the position relationship between the terminal and the target satellite after the user moves.
In the embodiment of the application, the terminal can guide the user to adjust the position relationship between the terminal and the target satellite through the satellite finding guiding interface, so that the terminal can quickly establish communication connection with the satellite, and the terminal can quickly send or receive satellite information.
Optionally, the star finding guiding interface further includes a star finding prompt message, where the star finding prompt message is used to prompt the direction of the user mobile terminal.
Optionally, the star-finding guiding interface comprises a first star-finding guiding interface and a second star-finding guiding interface; the first satellite searching guide interface comprises a first satellite identifier and a first alignment area, wherein the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition, the first satellite identifier is positioned in the first alignment area; the second satellite searching guide interface comprises a second satellite identifier and a second alignment area, wherein the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is positioned in the second alignment area.
Optionally, the display unit 1401 is specifically configured to display the first star finding guiding interface.
The processing unit 1402 is specifically configured to update the display position of the first satellite identifier in response to a leftward movement operation or a rightward movement operation of the terminal by the user.
The display unit 1401 is specifically configured to display the second satellite searching guiding interface when the first satellite identifier is located in the first alignment area.
The processing unit 1402 is specifically configured to update the display position of the second satellite identifier in response to an upward movement operation or a downward movement operation of the terminal by the user.
Optionally, the display unit 1401 is specifically configured to display the second star finding guiding interface.
The processing unit 1402 is specifically configured to update the display position of the second satellite identifier in response to an upward movement operation or a downward movement operation of the terminal by the user.
The display unit 1401 is specifically configured to display the first satellite searching guiding interface when the second satellite identifier is located in the second alignment area.
The processing unit 1402 is specifically configured to update the display position of the first satellite identifier in response to a leftward movement or a rightward movement operation of the terminal by the user.
Optionally, the satellite finding guiding interface comprises a first satellite identifier and a first alignment area, and a second satellite identifier and a second alignment area; the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and is positioned in the first alignment area when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition; the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is located in the second alignment area.
Optionally, the processing unit 1402 is specifically configured to update the display position of the first satellite identifier in response to a leftward movement operation or a rightward movement operation of the terminal by the user; and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
Optionally, when the display position of the first satellite identifier is located outside the first alignment area, the first alignment area is displayed in a first color; when the display position of the first satellite mark is positioned in the first alignment area, the first alignment area is displayed in a second color, and the first color is different from the second color.
Optionally, when the display position of the second satellite identifier is located outside the second alignment area, the second alignment area is displayed in a third color; when the display position of the second satellite mark is positioned in the second alignment area, the second alignment area is displayed in a fourth color, and the third color is different from the fourth color.
Optionally, the display unit 1401 is further configured to, when the terminal is configured to send the first satellite message, display a satellite message editing interface, where the satellite message editing interface is used for the user to input the content of the first satellite message, in response to an operation of creating the satellite message or an operation of replying to the satellite message by the user before displaying the satellite finding guiding interface.
Optionally, the display unit 1401 is specifically configured to display a star finding guidance interface in response to a user sending operation of the first satellite message.
Optionally, the display unit 1401 is specifically configured to display a satellite finding guidance interface in response to an operation of receiving a satellite message by a user.
Optionally, the transceiver unit 1403 is further configured to send a common message to the base station; and receiving a response message of failure of sending the common message.
The display unit 1401 is specifically configured to display a star finding guidance interface in response to a response message of failure in transmission of a normal message.
Optionally, the processing unit 1402 is further configured to determine a change in position after the terminal transmits the first satellite message in response to a user transmitting the second satellite message.
The transceiver 1403 is further configured to send a second satellite message to the target satellite if the position change after the terminal sends the first satellite message is smaller than the first threshold, and the satellite finding guiding interface is not displayed.
Optionally, the transceiver unit 1403 is further configured to receive a response message that the first satellite message fails to be sent.
The display unit 1401 is further configured to display a star finding guidance interface according to a response message of the failure of the first satellite message transmission.
In the embodiment of the present application, the operations performed by the units in the terminal are similar to those described in the embodiments shown in fig. 3 to 13B, and are not repeated here.
In another embodiment of the present application, there is also provided a computer-readable storage medium having stored therein computer-executable instructions which, when executed by a processor of a terminal, perform the steps performed by the terminal device of fig. 3 to 13B described above.
In another embodiment of the present application, there is also provided a computer program product comprising computer program code for, when executed on a computer, the computer device performing the steps performed by the terminal of fig. 3 to 13B described above.
In another embodiment of the application, there is also provided a chip system including one or more interface circuits and one or more processors; the interface circuit and the processor are interconnected through a circuit; the interface circuit is used for receiving signals from the memory of the terminal and sending signals to the processor, and the signals comprise computer instructions stored in the memory; when the processor executes the computer instructions, the terminal performs the steps performed by the terminal device in fig. 3 to 13B described above. In one possible design, the chip system may further include a memory to hold program instructions and data necessary for the control device. The chip system can be composed of chips, and can also comprise chips and other discrete devices.
In the several embodiments provided in the present application, it should be understood that the disclosed systems, devices, and methods may be implemented in other manners. For example, the apparatus embodiments described above are merely illustrative, e.g., the division of elements is merely a logical functional division, and there may be additional divisions of actual implementation, e.g., multiple elements or components may be combined or integrated into another system, or some features may be omitted, or not performed. Alternatively, the coupling or direct coupling or communication connection shown or discussed with each other may be an indirect coupling or communication connection via some interfaces, devices or units, which may be in electrical, mechanical or other form.
The units described as separate units may or may not be physically separate, and units shown as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the units may be selected according to actual needs to achieve the purpose of the solution of this embodiment.
In addition, each functional unit in the embodiments of the present application may be integrated in one processing unit, or each unit may exist alone physically, or two or more units may be integrated in one unit. The integrated units described above may be implemented in whole or in part by software, hardware, firmware, or any combination thereof.
When the integrated unit is implemented in software, it may be implemented in whole or in part in the form of a computer program product. The computer program product includes one or more computer instructions. When loaded and executed on a computer, produces a flow or function in accordance with embodiments of the present application, in whole or in part. The computer may be a general purpose computer, a special purpose computer, a computer network, or other programmable apparatus. The computer instructions may be stored in a computer-readable storage medium or transmitted from one computer-readable storage medium to another computer-readable storage medium, for example, the computer instructions may be transmitted from one website, computer, server, or data center to another website, computer, server, or data center by a wired (e.g., coaxial cable, fiber optic, digital subscriber line (digital subscriber line, DSL)) or wireless (e.g., infrared, wireless, microwave, etc.). The computer readable storage medium may be any available medium that can be accessed by a computer or a data storage device such as a server, data center, etc. that contains an integration of one or more available media. The usable medium may be a magnetic medium (e.g., a floppy disk, a hard disk, a magnetic tape), an optical medium (e.g., a DVD), or a semiconductor medium (e.g., a Solid State Disk (SSD)), or the like.

Claims (18)

1. A method for message transmission, applied to a terminal, comprising:
displaying a satellite finding guiding interface, wherein the satellite finding guiding interface comprises a satellite identifier, and the display position of the satellite identifier on the satellite finding guiding interface is used for indicating the position relationship between the terminal and a target satellite;
responding to the mobile operation of the user to the terminal, and updating the display position of the satellite identifier;
and if the position relation between the terminal and the target satellite after the movement meets the message transmission condition, sending a first satellite message to the target satellite or receiving the first satellite message from the target satellite.
2. The method of claim 1, wherein the star-finding guidance interface further comprises a star-finding cue for cue a user to move the terminal in a direction.
3. A method according to claim 1 or 2, characterized in that,
the star finding guiding interface comprises a first star finding guiding interface and a second star finding guiding interface;
the first satellite searching guide interface comprises a first satellite identifier and a first alignment area, the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in the azimuth angle, and when the position relation between the terminal and the target satellite in the azimuth angle meets the message transmission condition, the first satellite identifier is positioned in the first alignment area;
The second satellite searching guide interface comprises a second satellite identifier and a second alignment area, the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in a pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is located in the second alignment area.
4. The method of claim 3, wherein the step of,
the star finding guiding interface is displayed; the method for updating the display position of the satellite identifier in response to the mobile operation of the user on the terminal specifically comprises the following steps:
displaying the first satellite finding guiding interface, and responding to the leftward movement operation or the rightward movement operation of the user on the terminal to update the display position of the first satellite identifier;
displaying the second satellite finding guiding interface when the first satellite identifier is positioned in the first alignment area;
and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
5. The method of claim 3, wherein the step of,
the star finding guiding interface is displayed; the method for updating the display position of the satellite identifier in response to the mobile operation of the user on the terminal specifically comprises the following steps:
Displaying the second satellite finding guiding interface, and responding to the upward movement operation or the downward movement operation of the user on the terminal, and updating the display position of the second satellite identifier;
displaying the first satellite finding guiding interface when the second satellite identifier is positioned in the second alignment area;
and in response to the leftward or rightward movement operation of the terminal by the user, updating the display position of the first satellite identifier.
6. A method according to claim 1 or 2, characterized in that,
the satellite finding guiding interface comprises a first satellite identifier and a first alignment area, and a second satellite identifier and a second alignment area;
the first satellite identifier is used for indicating the position relation between the terminal and the target satellite in azimuth, and when the position relation between the terminal and the target satellite in azimuth meets the message transmission condition, the first satellite identifier is positioned in the first alignment area;
the second satellite identifier is used for indicating the position relation between the terminal and the target satellite in the pitch angle, and when the position relation between the terminal and the target satellite in the pitch angle meets the message transmission condition, the second satellite identifier is located in the second alignment area.
7. The method according to claim 6, wherein the updating the display position of the satellite identifier in response to the mobile operation of the terminal by the user specifically comprises:
responding to the leftward movement operation or the rightward movement operation of the user on the terminal, and updating the display position of the first satellite identifier; or alternatively, the first and second heat exchangers may be,
and updating the display position of the second satellite identifier in response to the upward movement operation or the downward movement operation of the terminal by the user.
8. The method according to any one of claims 3 to 7, wherein,
when the display position of the first satellite mark is positioned outside the first alignment area, the first alignment area is displayed in a first color; when the display position of the first satellite mark is located in the first alignment area, the first alignment area is displayed in a second color, and the first color is different from the second color.
9. The method according to any one of claims 3 to 8, wherein,
when the display position of the second satellite mark is positioned outside the second alignment area, the second alignment area is displayed in a third color; and when the display position of the second satellite mark is positioned in the second alignment area, the second alignment area is displayed in a fourth color, and the third color is different from the fourth color.
10. The method according to any of claims 1-9, wherein when the terminal is used to send the first satellite message, the method further comprises, prior to the displaying of the star finding guidance interface:
and responding to the operation of newly building the satellite message or replying the satellite message by the user, displaying a satellite message editing interface, wherein the satellite message editing interface is used for inputting the content of the first satellite message by the user.
11. The method of claim 10, wherein displaying the star finding guidance interface specifically comprises:
and responding to the sending operation of the user on the first satellite message, and displaying the star finding guiding interface.
12. The method according to any one of claims 1-9, wherein said displaying the satellite finding guidance interface when the terminal is used for receiving the first satellite message, comprises:
and responding to the operation of receiving the satellite message by the user, and displaying the star finding guiding interface.
13. The method according to any of claims 1-9, wherein when the terminal is used to send the first satellite message, the method further comprises, prior to the displaying of the star finding guidance interface:
Sending a common message to a base station;
receiving a response message of the failure of sending the common message;
the displaying the star finding guiding interface specifically includes:
and responding to the response message of the failure of the common message sending, and displaying the star finding guiding interface.
14. The method according to any one of claims 1-11, 13, wherein after sending the first satellite message, the method further comprises:
determining a position change after the terminal transmits the first satellite message in response to a user transmitting operation of a second satellite message;
and if the position change after the terminal sends the first satellite message is smaller than a first threshold value, sending the second satellite message to the target satellite, and not displaying the satellite finding guiding interface.
15. The method of any of claims 1-11, 13-14, wherein after transmitting the first satellite message to the target satellite, the method further comprises:
receiving a response message of the failure of the first satellite message transmission;
and displaying the star finding guiding interface according to the response message of the failure of the first satellite message transmission.
16. A terminal, comprising: a transceiver, a processor and a memory, the transceiver and the processor being coupled with the memory, the memory for storing a program or instructions that, when executed by the processor, cause the terminal to perform the method of any one of claims 1 to 15.
17. A computer readable storage medium having instructions stored therein which, when run on a terminal, cause the terminal to perform the method of any of claims 1 to 15.
18. A computer program product, characterized in that the computer program product comprises computer program code which, when run on a computer, causes the computer to perform the method of any one of claims 1 to 15.
CN202210270407.0A 2022-03-18 2022-03-18 Message transmission method and corresponding terminal Pending CN116806013A (en)

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US18/552,285 US20240048651A1 (en) 2022-03-18 2023-03-10 Message transmission method and corresponding terminal
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CN106569229A (en) * 2016-11-07 2017-04-19 工业和信息化部电信研究院 Method and device for determining ephemeris information of visible satellite in LTE standard
CN111026167A (en) * 2019-12-24 2020-04-17 深圳市星网荣耀科技有限公司 Star finding system and star finding and aiming method
CN113271558A (en) * 2021-05-08 2021-08-17 东方红卫星移动通信有限公司 Internet of things information transmission method, terminal and system in low-orbit satellite Internet of things
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CN117278109A (en) * 2023-11-20 2023-12-22 哈尔滨工业大学(深圳)(哈尔滨工业大学深圳科技创新研究院) Satellite on-orbit safety anomaly identification method for far-sea wind power plant
CN117278109B (en) * 2023-11-20 2024-03-01 哈尔滨工业大学(深圳)(哈尔滨工业大学深圳科技创新研究院) Satellite in-orbit security anomaly identification method, system and computer readable storage medium

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